COMBUSTION CHAMBER OF AIRCRAFT ENGINE OR POWER GAS-TURBINE ENGINE Russian patent published in 1997 - IPC

Abstract RU 2094705 C1

FIELD: aircraft and stationary power plants. SUBSTANCE: combustion chamber has multi-injector device with two-loop fuel manifold. Number of injectors is determined from formula. Injectors are made as dual-orifice injectors: inner orifice for fuel and outer orifice for air. EFFECT: enhanced efficiency. 3 cl, 8 dwg

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RU 2 094 705 C1

Authors

Sigalov Ju.V.

Rudakov O.A.

Efimov E.V.

Gurskij S.Eh.

Mitrofanov V.A.

Fedorov A.M.

Dates

1997-10-27—Published

1994-04-28—Filed